TECHNICAL FIELD
[0001] The present invention relates to a sealed type compressor, more particularly, an
improvement in the structure of a sealed type compressor.
BACKGROUND ART
<Overall Arrangement of Rotary Compressor>
[0002] An overall arrangement of a rotary compressor will be described with reference to
Fig. 6. Fig. 6 is a vertical sectional view representing an overall arrangement of
a rotary compressor. At the lower end side of a casing 1 is arranged a compression
element 7 corresponding to induction pipes 5a and 5b for compressing the input working
fluid. In addition, a drive element 8 for driving compression element 7 is arranged
thereabove, occupying substantially the entire region of the internal space. At the
internal space defined by a lower lid 4 at the lower end region of casing 1, an oil
reservoir 9 storing a lubricant O is formed. A storage space 10 for storing compressed
working fluid is formed at another space.
<Compression Element 7>
[0003] Compression element 7 is configured having a cylinder chamber at an upper stage and
at a lower stage, i.e. two cylinder chambers. Compression element 7 includes an upper
cylinder 12a with a cylinder chamber 11a having a circular transverse cross section,
a lower cylinder 12b with a cylinder chamber 11b having a circular transverse cross
section, and a middle plate 18 therebetween. On both upper and lower surfaces of upper
cylinder 12a and lower cylinder 12b are provided an upper bearing 13 having a boss-shaped
bearing portion 13a at its center and a lower bearing 14 also having a boss-shaped
bearing portion 14a at its center, fastened by a plurality of bolts 15 to set cylinder
chambers 11a and 11b at a sealed state.
[0004] Upper cylinder 12a and lower cylinder 12b are supported at a horizontal state in
casing 1. An outlet 13c is provided at upper bearing 13. A front muffler 16 is secured
to upper bearing 13 around bearing portion 13a so as to form an annular gap with respect
to bearing portion 13a of upper bearing 13. Furthermore, an outlet 14c is provided
at lower bearing 14. In addition, a rear muffler 17 that partitions oil reservoir
9 from the discharge space is secured to lower bearing 14 around bearing portion 14a
of lower bearing 14.
[0005] An upper piston 19a and a lower piston 19b are arranged at cylinder chambers 11a
and 11b of upper cylinder 12a and lower cylinder 12b, respectively. Upper and lower
pistons 19a and 19b are arranged at the outer circumference of eccentric portions
20a and 20b of a crankshaft 26.
<Drive Element 8>
[0006] Drive element 8 includes an electric motor constituted of a stator 24 and a rotor
25. Stator 24 is fixedly-supported to an inner wall of a middle cylindrical body 2
in a casing 1. A rotor 25 is disposed concentrically with and at the inner side of
stator 24 with a predetermined circumferential gap therebetween. The upper half portion
of crankshaft 26 is mounted at the inner side of rotor 25 to rotate integrally about
the shaft center. The lower half portion of crankshaft 26 is fit-supported rotatably
by both bearing portions 13a and 14a of upper bearing 13 and lower bearing 14.
[0007] An oil channel 26a extending along the shaft center direction is formed at crankshaft
26. A centrifugal oil pump 27 is attached at the lower end of crankshaft 26. Oil pump
27 is constantly immersed in lubricant O of oil reservoir 9 to draw up lubricant O
into oil channel 26a according to the rotation of crankshaft 26. The lubricant is
supplied through a plurality of lubricant supply holes 26b provided at crankshaft
26 to each slidable site of compression element 7 and drive element 8.
[0008] The supply of lubricant towards bearing portion 14a of lower bearing 14 will be described
hereinafter with reference to Figs. 7 and 8. Fig. 7 is a perspective view of lower
bearing 14, viewed from the bearing portion 14a side. Fig. 8 is a vertical sectional
view of lower bearing 14. As shown in Fig. 7, a communicating groove 14c is provided
at the inner circumferential face of bearing portion 14a of lower bearing 14, spanning
from the upper end to the lower end in parallel with crankshaft 26 along the shaft
center direction. The lubricant output from lubricant supply opening 26b provided
at crankshaft 26 runs along the outer surface of crankshaft 26 (F1) via communicating
groove 14c to be supplied to the region between bearing portion 14a and the sliding
face of crankshaft 26 (F2).
[0009] Since communicating groove 14c has both the upper and lower ends open as shown in
Fig. 8, not all the lubricant (F1) output from lubricant supply hole 26b is supplied
to the region between bearing portion 14a and the sliding face of crankshaft 26. A
portion of the lubricant (F3) is discharged to oil reservoir 9 without being used
as the lubricant.
[0010] It is to be noted that oil pump 27 draws up an amount of lubricant, a portion that
will discharged to oil reservoir 9 without being used for lubrication, in addition
to the amount required for lubrication towards respective sliding sites, causing futile
pump loss. Patent Document 1 set forth below can be cited as a document disclosing
a rotary compressor such as that shown in Fig. 4. In addition, Non-Patent Document
1 can be cited as a document disclosing the art of a rotary compressor oil supply
system.
[0011] Patent Document 1: Japanese Patent Laying-Open No.
2004-324652
DISCLOSURE OF THE INVENTION
PROBLEMS TO BE SOLVED BY THE INVENTION
[0013] The problem to be solved by the invention arises from the fact that the oil supply
groove provided at the lower bearing employed in a sealed type compressor is a communicating
groove with both the upper and lower ends open. Futile pump loss occurs since the
oil pump must draw up the lubricant that is merely to be output to the oil reservoir
without being supplied to the lower bearing even though there is sufficient lubricant
to be discharged to the oil reservoir. Thus, the present invention is directed to
solving the above-described problem, and provides a sealed type compressor allowing
improvement in the oil supply capability of the oil pump to suppress occurrence of
pump loss by reducing futile induction of lubricant at the oil pump.
MEANS FOR SOLVING THE PROBLEMS
[0014] A sealed type compressor according to the present invention has a compression element
and a drive element accommodated in a sealed vessel, and includes a crankshaft, a
piston disposed at an outer circumference of an eccentric portion of the crankshaft,
a cylinder defining a cylinder chamber where the piston is disposed, and an upper
bearing and a lower bearing having a bearing portion to support the crankshaft axially,
and sandwiching the cylinder and the piston from respective axial sides of the crankshaft.
[0015] The sealed type compressor includes an oil pump provided at a lower end of the crankshaft
to draw up a lubricant stored in an oil reservoir at the lower end portion of the
sealed vessel into an oil channel provided extending along a shaft center direction
of the crankshaft to provide lubrication to each sliding site of the compression element
and drive element, and an oil supply groove provided at a sliding face of the bearing
portion of the lower bearing, extending along an axial direction of the crankshaft
to supply the lubricant to the outer surface of the crankshaft.
[0016] The oil supply groove has one end side open at an end face of the cylinder side,
and the other end side closed at a lower end side of the crankshaft.
EFFECTS OF THE INVENTION
[0017] According to the sealed type compressor of the present invention, the oil supply
groove provided at the lower bearing is not a communicating groove open at the upper
and lower ends, and is closed at the lower end side of the crankshaft. As a result,
the lubricant supplied to the lower bearing is entirely applied to the lower bearing
without a portion being discharged to the oil reservoir.
[0018] Thus, by reducing futile induction of lubricant at the oil pump, the oil supply capability
of the oil pump can be improved to suppress occurrence of pump loss.
BRIEF DESCRIPTION OF THE DRAWINGS
[0019]
Fig. 1 is a perspective view of only a lower bearing employed in a rotary compressor
according to an embodiment of the present invention, viewed from the bearing portion
side.
Fig. 2 is a vertical sectional view of a lower bearing employed in a rotary compressor
according to an embodiment of the present invention.
Fig. 3 represents the oil supply rate to each sliding site when the lower bearing
of background art is employed, and the oil supply rate to each sliding site when the
lower bearing of the present embodiment is employed.
Fig. 4 is a sectional view representing the dimensional relationship of a lower bearing
employed in a rotary compressor according to an embodiment of the present invention.
Fig. 5 represents the relationship of X/L and the bearing temperature increase (°C)
of a lower bearing employed in a rotary compressor according to an embodiment of the
present invention.
Fig. 6 is a vertical sectional view representing an overall arrangement of a rotary
compressor according to background art.
Fig. 7 is a perspective view of only a lower bearing employed in a rotary compressor
according to background art, viewed from the bearing portion side.
Fig. 8 is a vertical sectional view of a lower bearing employed in a rotary compressor
according to background art.
DESCRIPTION OF THE REFERENCE SIGNS
[0020] 1 casing; 4 lower lid; 5a, 5b induction pipe; 7 compressor element; 8 drive element;
9 oil reservoir; 10 storage space; 11a, 11b cylinder chamber; 12a upper cylinder;
12b lower cylinder; 13 upper bearing; 13a bearing portion; 13c, 14c outlet; 14A lower
bearing; 14a bearing portion; 14b oil supply groove; 14c communicating groove; 15
bolt; 16 front muffler; 17 rear muffler; 18 middle plate; 19a upper piston; 19b lower
piston; 24 stator; 25 rotor; 26a oil channel; 26b lubricant supply hole; 27 oil pump;
O lubricant.
BEST MODES FOR CARRYING OUT THE INVENTION
[0021] Each of the embodiments of a sealed type compressor according to the present invention
will be described hereinafter with reference to the drawings. As an example of a sealed
type compressor of the present embodiment, an application of the present invention
to the rotary compressor set forth above in the background art will be described.
[0022] The rotary compressor of the present embodiment has the same basic arrangement as
the rotary compressor with a cylinder chamber at an upper stage and at a lower stage,
i.e. two cylinder chambers, described with reference to Fig. 6. A compression element
7 and a drive element 8 are accommodated in a casing 1 that is a sealed vessel. The
rotary compressor includes a crankshaft 26, an upper piston 19a and a lower piston
19b arranged at the outer circumference of eccentric portions 20a and 20b of crankshaft
26, an upper cylinder 12a and a lower cylinder 12b defining cylinder chambers 11a
and 11b where upper piston 19a and lower piston 19b are disposed, and bearing portions
13a and 14a to axial-support crankshaft 26.
[0023] There are further provided an upper bearing 13 and a lower bearing 14 sandwiching
upper cylinder 12a, upper piston 19a, lower cylinder 12b and lower piston 19b from
respective axial sides of crankshaft 26.
[0024] In addition, at the lower end of crankshaft 26 is provided an oil pump 27 to draw
up a lubricant O stored in an oil reservoir 9 at the lower end portion of casing 1
into an oil channel 26a provided so as to extend along the shaft center direction
of crankshaft 26 to provide lubrication to each sliding site of compression element
7 and drive element 8, according to the rotation of crankshaft 26.
[0025] In the following description, elements identical to or corresponding to those of
the rotary compressor described with reference to Fig. 6 have the same reference characters
allotted, and description thereof will not be repeated. Only the characteristic features
of the present invention will be described in detail hereinafter.
[0026] Referring to Figs. 1 and 2, the characteristic portion of the rotary compressor of
the present embodiment will be described. Fig. 1 is a perspective view of only lower
bearing 14A employed in the rotary compressor of the present embodiment, viewed from
the bearing portion 14a side. Fig. 2 is a vertical sectional view of lower bearing
14A.
[0027] As shown in Fig. 1, an oil supply groove 14b is provided at the inner circumferential
face of bearing portion 14a of lower bearing 14A. Oil supply groove 14b has one end
side open at the end face of the cylinder 12b side (refer to Fig. 6).
[0028] The other end side of oil supply groove 14b extends to a region partway of bearing
portion 14a at the lower end side of crankshaft 26.
[0029] The lubricant (F1) discharged from lubricant supply opening 26b provided at crankshaft
26 (refer to Fig. 6) runs along the outer surface of crankshaft 26 via oil supply
groove 14b to be supplied to the region between bearing portion 14a and the sliding
face of crankshaft 26 (F2).
[0030] As shown in Fig. 2, oil supply groove 14b is not a communicating groove open at the
lower end, and extends to a region only as far as partway of bearing portion 14a at
the lower end side of crankshaft 26. Since oil supply groove 14b takes a closed state
at the lower end side of crankshaft 26, the lubricant supplied to lower bearing 14A
is entirely applied to lower bearing 14A without a portion being discharged to oil
reservoir 9 (refer to Fig. 6). Fig. 1 represents a configuration in which oil supply
groove 14b extends to a region only as far as partway of bearing portion 14a at the
lower end side of crankshaft 26. In the case where the groove is provided extending
from the upper end to the lower end of crankshaft 26, likewise of communicating groove
14c shown in Fig. 7, a structure of closing the lower end side of the oil supply groove
can be adapted by providing another member such as a plate member at the lower end
of the groove.
[0031] Fig. 3 represents the oil supply rate (cc/min) of the lubricant to each sliding site
corresponding to the case where lower bearing 14 of the background art shown in Fig.
8 is employed, and the oil supply rate (cc/min) to each sliding site corresponding
to the case where lower bearing 14A of the present embodiment is employed. The oil
supply rate (cc/min) of the lubricant supplied to the upper bearing (A1), upper piston
19a (A2), and lower piston 19b (A3) does not vary between the background art and the
present embodiment.
[0032] However the oil supply rate (cc/min) of lubricant to the lower bearing (A4) is greatly
reduced in the present embodiment, as compared to that of the background art. This
is because the lubricant supplied to lower bearing 14A of the present embodiment is
entirely applied to lower bearing 14 without being partially discharged to oil reservoir
9 (refer to Fig. 6), as described before, avoiding unnecessary drawing up of lubricant
by oil pump 27.
[0033] The effect on the bearing performance when oil supply groove 14b is closed at the
lower end side of bearing portion 14a will be studied from the standpoint of
<bearing friction loss> and <cooling performance of bearing>.
<Bearing Friction Loss>
[0034] The most critical factor in the issue of the oil supply rate involved in the reliability
of a bearing is the cooling performance. It is possible to appraise the cooling performance
by estimating how much the oil temperature rises by the generated bearing friction
loss. The bearing friction loss W can be expressed by equation 1 set forth below,
where L is the overall bearing length, r the bearing radius, µ the oil viscosity,
u the sliding rate, C the clearance, and δ the oil film clearance. Assuming that overall
bearing length L, bearing radius r, oil viscosity µ and sliding rate u are constants
in equation 1, bearing friction loss W will rapidly increase when the oil film clearance
δ approaches zero.

(where λ = 1 - (δ/C))
<Cooling Performance of Bearing>
[0035] In the case where it is assumed that the oil supply rate to the bearing varies linearly
when the length of the oil supply groove is shortened, and that the oil film clearance
in such a case also varies linearly in proportion to the oil supply rate, a shorter
length of the oil supply groove causes reduction in the oil supply rate, which in
turn reduces the oil film clearance to increase the bearing friction loss. It is to
be noted that the bearing friction loss tends to increase suddenly when the oil film
clearance becomes small, as indicated by equation 1 set forth above. Therefore, when
the oil film clearance becomes small, the temperature of the bearing rises significantly
since cooling is effected with a smaller amount of lubricant corresponding to the
greater bearing friction loss.
[0036] The relationship between the ratio (X/L) of the length of the oil supply groove (X)
to the entire length of the bearing (L) and the bearing temperature increase will
be described with reference to Figs. 4 and 5. Fig. 4 is a sectional view representing
the dimensional relationship of lower bearing 14A. Fig. 5 represents the relationship
between X/L and the bearing temperature increase (°C). As shown in Fig. 5, the bearing
temperature is maintained below approximately 20 degrees when the X/L is from 0.4
to 1. The bearing temperature is also below approximately 40 degrees when the X/L
is from 0.2 to 0.4. However, when the X/L becomes lower than 0.2, the oil film clearance
becomes small to cause increase of the bearing friction loss. As a result, the cooling
performance is greatly degraded. It is therefore desirable that the X/L is in the
range from 0.2 to 0.8, preferably from 0.6 to 0.8.
[0037] Although the embodiment has been described based on the case where the present invention
is applied to a rotary compressor having a cylinder at an upper stage and at a lower
stage, i.e. two cylinders, the present invention is also applicable to a rotary compressor
having a cylinder at one stage. Moreover, the structure based on the present invention
is widely applicable, not only to rotary compressors, but to other sealed type compressors
having a similar compression element structure.
[0038] It should be understood that the embodiments disclosed herein are illustrative and
non-restrictive in every respect. The scope of the present invention is defined by
the appended claims, and all changes that fall within the limits and bounds of the
claims, or equivalence thereof are intended to be embraced by the claims.
1. A sealed type compressor having a compression element (7) and a drive element (8)
accommodated in a sealed vessel (1), the sealed type compressor including a crankshaft
(26), a piston (19a, 19b) disposed at an outer circumference of an eccentric portion
(20a, 20b) of said crankshaft (26), a cylinder (12a, 12b) defining a cylinder chamber
(11a, 11b) where said piston (19a, 19b) is disposed, and an upper bearing (13) and
a lower bearing (14) having a bearing portion (13a, 13b) to support said crankshaft
axially, and sandwiching said cylinder (12a, 12b) and said piston (19a, 19b) from
respective axial sides of said crankshaft (26), said sealed type compressor comprising:
an oil pump (27) provided at a lower end of said crankshaft (26) to draw up a lubricant
(O) stored in an oil reservoir (9) at a lower end portion of said sealed vessel (1)
into an oil channel (26a) provided extending in a shaft center direction of said crankshaft
(26) to provide lubrication at each sliding site of the compression element (7) and
drive element (8), according to rotation of said crankshaft (26), and
an oil supply groove (14b) provided at a sliding face of said bearing portion (14a)
of said lower bearing (14), extending along an axial direction of said crankshaft
(26) to supply the lubricant to an outer surface of said crankshaft (26),
said oil supply groove (14b) having one end side open at an end plane of said cylinder
(12b) side and an other end side of said oil supply groove (14b) closed at a lower
end side of said crankshaft (26).
2. The sealed type compressor according to claim 1, wherein the other end side of said
oil supply groove (14b) extends to a region partway of said bearing portion (14a).
3. The sealed type compressor according to claim 1, wherein a value of X/L is set in
a range from 0.2 to 1.0, where X is a length of said oil supply groove (14b) and L
is an overall bearing length L of said bearing portion (14a).